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17
CHAPTER 2: WAVEGUIDE ANALYSIS METHODS
2.1 Introduction
This chapter discusses the types of the waveguides and the behavior of light from the
point of view of ray optics and electromagnetic theory, followed by a brief treatment on
simulation techniques. Subsequently, the basic idea of the Finite Difference Method
(FDM) will be elaborated further in Section 2.2 as will the effects of the boundary
conditions. This is followed by a discussion on Beam Propagation Method (BPM) and
how FDM is employed in BPM. The last section describes the Coupled Mode Theory
(CMT) which is used to deal with coupling activities between two closely spaced
waveguides.
2.2 Planar Waveguides
Planar waveguides are optical components that allow the confinement of light within
certain boundaries by total internal reflection. Typically, there are three main types of
basic waveguides structure commonly used in silica-on-silicon platform: ridge, rib, and
buried waveguide as illustrated in Figure 2.1 [1]. In Figure 2.1, the waveguide core
layer is shown in dark blue whereas the waveguide cladding is shaded in light blue.
18
Figure 2.1: Three planar waveguide types: (a) ridge waveguide; (b) rib waveguide;
and (c) buried waveguide.
The core layer has a higher refractive index than its surrounding cladding layer in order
to keep the light (in the form of photon) well confined in the waveguide. It thus can be
said that the cladding is treated as a protective layer to guide the light within the core
with minimum losses and throughout this work, the buried waveguide is used. The
mechanism of light guidance in the waveguide will be discussed in the next section.
2.2.1 Light Behavior from the Point of View of Ray Optics
Light behavior within a planar waveguide can be outlined and analyzed
from the point of view of ray optics. Consider the planar waveguide illustrated in
Figure 2.1(c), where core layer (dark blue) is enclosed or sandwiched by
cladding layer (light blue). We assume n1 to represent the refractive index value
of the core layer and n2 corresponding to the refractive index value of the
cladding layer. In addition, we also assume that n1 is higher than n2. Thus, the
propagation of light through the planar waveguide by Total Internal Reflection
(TIR) can be intuitively understood by the use of the ray optics model.
Light source
(a) (b) (c)
Core Cladding
19
As shown earlier, the flow of light within the waveguide is governed by Snell’s
Law. Snell’s Law is used to describe the relationship that governs the light
propagation, where incident angle 1 of light in a medium with index n1 impinge
on the boundary of a dissimilar medium with index n2, resulting the light is
refracted at angle of 2 as depicted in Figure 2.2 (a).
The relationship that governs the light propagation that was derived from Snell’s
Law is shown below [2];
2211 sinsin nn (2.1)
is measured with respect to the normal of interface of two different medium.
In order to confine light within the waveguide, n1 has to be larger than n2.
Furthermore, if 2 becomes 90o, a condition termed total internal reflection (TIR)
occurs, where incident light impinging on the boundary is reflected back into
same medium. The incident angle, 1 that allow for this situation is called the
critical angle, c . As such, equation 2.1 can be simplified to [2];
n1
n2
1
2 If 1 > c
cladding, n2
cladding, n2
core, n1
c
n n1
n2
n2
(a) (b) (c)
Figure 2.2: (a) Reflection and refraction at a plane interface, (b) propagation of light
through optical waveguide by total internal reflection (TIR), (c) refractive index
profile of the optical waveguide
x
20
)(sin1
21
1n
n (2.2)
It can be seen from Fig. 2.2(b), if incident angle 1 exceed c , light will continue
to be reflected at the interface and subsequently guided via TIR in the core layer
[2]. The distribution of the refractive index which core layer has higher index
value is illustrated in Fig. 2.2(c). It is found that a small portion of guided light is
accumulated outside of core region. It is called evanescent field and this is very
useful for energy transfer to another adjacent waveguide.
2.2.2 Light Behavior from the Point of View of Electromagnetic Theory
Although the ray optics approach can be utilized for qualitative description and
basic understanding for light behavior within the waveguide, the technique lacks
the information and ability to explain the relationship between the electric and
magnetic field distribution. In many applications such as optical coupling, it is
essential to know the distribution of optical field or intensity within the
waveguide. Therefore it is necessary to include the more rigorous waveguide
treatment based on Maxwell’s equations.
The electromagnetic theory of light applied to the planar waveguide is
described by Maxwell’s equations [3-5]. We start the Maxwell’s equations by
assuming that the light is penetrating via a non-conductive dielectric
(conductivity 0 ), isotropic, non-magnetic (magnetic permeability o ),
and linear medium ( ED ). Therefore, Maxwell’s equations are reduced to [5]:
21
t
HEX o
(2.3)
t
EnHX o
2 (2.4)
where E
and H
are the electric and magnetic fields respectively, o is the free
space permeability, o is the permittivity of the free space and n is the refractive
index of the light propagation medium. Under the conditions mentioned above, it
is noted that div E and div H are equal to zero.
For an optically inhomogeneous medium with the refractive index
changes only in the transverse direction, )(rnn and using Maxwell’s
equations (2.3) and (2.4), we obtain the following wave equations for E
and H
[5]:
0)1
(2
222
2
2
t
EnEn
nE oo
(2.5)
0)(1
2
222
2
2
t
HnHXXn
nH oo
(2.6)
The above equations indicate that the Cartesian components of the
electric field vector xE , yE and zE and magnetic field vector xH , yH and zH are
coupled in an inhomogeneous medium. In this regard, a scalar wave equation for
each component cannot be established as in the case of a homogeneous medium.
However, the adequate solution to the inhomogeneous wave equations (2.5) and
(2.6) for monochromatic wave is described by the form [5]:
22
)(),(),( ztieyxEtrE
(2.7)
)(),(),( ztieyxHtrH
(2.8)
where is the propagation constant and being the angular frequency of the
wave. These two expressions indicate the electromagnetic field for a propagating
mode. By applying the solution for planar waveguide given in equations (2.7)
and (2.8) to Maxwell’s equations in equations (2.3) and (2.4), and taking their x,
y and z components as shown in Figure 2.3, we obtain the following expressions
[5]:
xoyz HjEj
y
E
(2.9)
zoxy
Hjy
E
x
E
(2.10)
yoz
x Enjx
HHj 2
(2.11)
xoyz EnjHj
y
H 2
(2.12)
zoxy
Enjy
H
x
H2
(2.13)
yoz
x Hjx
EEj
(2.14)
23
In the case of wave guiding confined to one direction (one dimension
confinement), the confinement is assumed to be in x-direction within the core
layer. In addition, the upper and lower cladding layers are respectively assumed
to be infinity. Furthermore, the light is assumed to propagate in z-direction and
the waveguide is also assumed no dependence in y-direction. Therefore the
electric and magnetic fields in the planar waveguide show independence on y-
direction and by setting 0
y
E
and 0
y
H
equations (2.9) to (2.14) can be
simplified to [5]:
xoy HE (2.15)
zo
yHj
x
E
(2.16)
yoz
x Exnjx
HHj )(2
(2.17)
xoy ExnH )(2 (2.18)
zo
yExnj
x
H)(2
(2.19)
yoz
x Hjx
EEj
(2.20)
x z
y
Core, n1
Upper cladding, n3
Lower cladding, n2
0
-d
Figure 2.3: The basic structure of the slab waveguide where the core layer is
sandwiched between upper cladding and lower cladding
24
The first three equations only involve yE , xH and zH and the last three
expressions involve xE , zE and yH . The first set of equations, equations (2.15)
to (2.17) corresponds to the TE (transverse electric) modes as TE modes only
contain the transverse component ( yE ) with respect to the direction of
propagation z, thus 0zE . Meanwhile the second set of equations are denoted as
TM (transverse magnetic) modes which having the non-vanishing value of xE ,
zE and yH . Similarly, the magnetic fields have only a transverse component
( yH ) and no magnetic field along the z direction, hence 0zH .
As discussed earlier, the propagation of light within a planar waveguide
may be described in terms of TE modes and TM modes. We first consider the
TE modes by substituting xH and zH components from equations (2.15) and
(2.16) into equation (2.17) to obtain the TE wave equation for yE as [5]
0])([ 222
2
2
yo
yExnk
dx
E (2.21)
where the free space wave number is given by, ooook .
The analysis so far is valid for an arbitrary x-dependent profile. Referring
back to Figure 2.3, the core layer which has a refractive index value, 1n is
sandwiched between two cladding layers which have refractive index values
2n and 3n . They are separated by planar boundaries perpendicular to the x-axis.
In this case, z is the propagation axis for the light beam. In order to confine the
light beam to within the waveguide, we assume 321 nnn . The plane
25
0x corresponds to the upper cladding-core boundary and the core-lower
cladding boundary is located at dx . Thus the core thickness is d . The
specific index profile of planar waveguide structures as depicted in Figure. 2.3 is
utilized and given as below:
;
;
;
)(
3
2
1
n
n
n
xn
0
0
x
dx
xd
(2.22)
The mode that is mainly confined within the core layer is denoted as guided
modes and its power decay exponentially in the cladding. To fulfill boundary
condition at 0 xd , the propagation constant associated with a particular
mode must have:
12 nknk oo (2.23)
In term of the refractive index, the effective index N of guided mode must be
located between 1n and 2n :
12 nNn (2.24)
where ok
N
. By imposing suitable boundary conditions, the wave equation
from (2.21) can be written as [5]:
26
02
12
2
y
yE
dx
E 0x (upper cladding) (2.25)
02
22
2
y
yE
dx
E dx (lower cladding) (2.26)
02
2
2
y
yE
dx
E 0 xd (cover) (2.27)
where the two parameters and are shown follows:
2
3
222
1 nko (2.28)
22
1
22 nko (2.29)
2
2
222
2 nko (2.30)
The solution of the electric field in the upper cladding, core and lower cladding
from equation (2.25) - (2.27) can be presented as [5]:
yEx
xixi
x
De
CeBe
Ae
2
1
dx
xd
x
0
0
(2.31)
where A , B , C and D are constant. Applying the continuity of yE and dx
dE yat
the boundaries 0x and dx yields the four equations that related to
constants A , B , C and D and propagation constant [5]:
ACB (2.32)
27
dididi DeCeBe 1 (2.33)
ACiBi 1 (2.34)
ddidi DeCeiBei 2
2
(2.35)
By solving equations (2.32) to (2.35), the following equation is acquired [5]:
21
21
1
tan d
(2.36)
The relation above can be considered as the dispersion relation for the
asymmetric step index planar waveguide and is a transcendental equation which
will determine the values of propagation constant. For the case of symmetric
step index planar waveguide ( 32 nn ), the transcendental equation is reduced to:
2
1
1
1
2
tan
d (2.37)
where 21 . The following descriptions only take account of asymmetric step
index planar waveguide. It is simple to modify the asymmetric expressions to
symmetric expression. In order to transcendental equation in equation (2.36) can
be universalized for any asymmetric step index waveguide, it is convenient to
introduce a set of normalized parameters:
28
2
2
2
1
2
2
2 )(
nn
nNb
; Normalized mode index, (2.38)
2
1
2
2
2
1 )( nndkV o ; Normalized core thickness/V-number, (2.39)
and 2
2
2
1
2
3
2
2 )(
nn
nna
; Asymmetry measure. (2.40)
The effective index N corresponding to a confined mode is in the range of
12 nNn whereas the normalized mode index b is bounded between 0 and 1.
As deduced from equation (2.39), the normalized core thickness V or V-number
is proportional to the thickness of core layer d and inversely proportional to
wavelength . The V-number includes all the waveguide parameters that will
determine the guidance behavior of the waveguide. On the other hand, the
asymmetry measured at a is zero in the case of symmetric waveguide,
thus 32 nn .
By rearranging the transcendental equation, it can be rewritten as the
function of propagation constant and in terms of the normalized parameters
[5]:
)1(
)(1
111tan
b
abb
b
ab
b
b
bV
(2.41)
The electric field in the three different regions can be determined after the
propagation constant is obtained numerically from equation (2.41):
29
yE
)(1
1
2
1
)sin(cos
)sin(cos
dx
x
eddA
xxA
Ae
dx
xd
x
0
0
(2.42)
Based on expressions above, the electrical fields decrease exponentially in upper
and lower cladding layers whilst the electrical fields vary sinusoidal in the core
layer. The solution for yE is completely validated except the constant A . It is
related to the energy carried by the mode.
Following the same procedure in determining yE , the magnetic field
component yH of a particular guided mode can be obtained. The wave equation
for TM propagation mode is identical to that obtained in TE, with the exception
that the magnetic field function has been established. TM wave equation for
yH is given as below:
0])([ 222
2
2
yo
yHxnk
dx
H (2.43)
The transcendental equation for TM waveguide is obtained in terms of
normalized parameters [5]:
)1(
)(11
1
1
1
1
1tan
b
abb
b
ab
b
b
bV
ba
ba
(2.44)
30
For the sake of simplicity, the a and b are respectively defined as
2
1
2
n
na and )1(
2
1
3bab a
n
n
. The solutions for the magnetic field
are [ref]:
yE
)(1
2
3
2
1
1
2
3
2
1
2
1
)sin(cos
)sin(cos
dx
x
edn
ndA
xn
nxA
Ae
dx
xd
x
0
0
(2.45)
The objective of the above discussion is to provide both qualitative and
quantitative picture about the guidance behavior of the waveguide. Nevertheless,
the theoretical treatment above is only restricted to the slab waveguide structure
as depicted in Figure 2.3. In the latter section, we will discuss the methods which
can be implemented for the guidance in channel waveguide. There are numerous
methods are available including effective index method [6, 7], Marcatili’s
method [8] and the FDM [9]. The first two techniques are considered as
analytical method and they will not be utilized throughout the work. It is found
that the analytical method is accurate than the numerical method. However the
FDM as a numerical method is employ in this work and will be elucidated at
next section.
31
2.3 The Finite Difference Method (FDM)
As discussed earlier, the electromagnetic fields propagating along the waveguide
are composed of guided modes, also can be addressed as eigenmodes, which are
dominated by transverse electric and magnetic field components with their
corresponding propagation constants. The behavior of these electromagnetic fields can
be analyzed and derived from the Maxwell’s equations. The analytical solution is
acquired by solving the Maxwell’s equations. Nevertheless, this is only for simple
waveguide geometries such as slab waveguides. For this reason, solving
electromagnetic problems for practical waveguide geometries requires the use of
numerical methods. Numerical methods are based on the approximation to the exact
solution and the standard that minimizes the error between the two. In the literature,
there are several numerical methods available such as FDM [10], Finite Element
Method (FEM) [11] and Method of Lines (MoL) [12] that can be used to solve the
eigenmode. Throughout this work, the FDM is employed to analyze the eigenmode
characteristics of an optical waveguide owing to its good numerical efficiency and
accuracy.
In the FDM, the cross-section of the waveguide is made discrete with a
rectangular grid of points which might be of identical or variable spacing as illustrated
in Figure 2.4. In each of the subdivisions, a two-dimensional wave equation is replaced
with appropriate Finite Difference relationship which is derived from a five-point
Taylor series formula [10]. Each grid of point is assigned to an arbitrary electric field
value. Due to the subdivisions being rectangular, thus the FDM is appropriate for
rectangular waveguide structure. As shown in Figure 2.4, by defining to be electric
field component to be calculated, the relationships are shown as below:
32
22
2 ),1(),(2),1(
x
nmnmnm
dx
, and (2.46)
22
2 )1,(),(2)1,(
y
nmnmnm
dy
(2.47)
where 2x and 2y are spacing between two grid of points in x and y direction
respectively.
There is a variety of boundary conditions that can be imposed at the edge of the analysis
window such as Dirichlet, Neumann [13] and Transparent Boundary Condition (TBC)
[14, 15]. The first and second boundary conditions for the calculation window are
categorized as fixed boundary condition. This means that the field (electric or magnetic
fields) is required to be set to zero at the boundary of the analysis window. It is a good
approximation if there is a large index discontinuity at the edge. Nevertheless, it
effectively reflects back the radiation to the analysis domain. To eliminate the back
reflections or incoming fluxes into the analysis window, the TBC is applied. It
effectively allows radiation to pass through the boundary freely and leave the analysis
domain without appreciable reflection. In this way, the unwanted interference in the
solution region (core layer) can be prevented [15].
x
n n+1 n-1
m
m+1
m-1
y
Figure 2.4: The cross-section of the waveguide is made discrete with a rectangular
grid of points which have identical spacing.
33
2.4 Finite Difference Beam Propagation Method
As discussed in the previous section, FDM shows an excellent way to solve the
waveguide eigenmode. Nevertheless it could not be utilized in solving the propagation
characteristic in integrated optics and fiber optics. Figure 2.5 shows the 3-Dimensional
Finite Difference as a plane rather than a ling along the z-axis.
The BPM is a widely used and indispensable numerical technique in today’s modeling
and simulation of evolution of electromagnetic fields in arbitrary inhomogeneous
medium. BPM is eligible to apply in complex geometries and automatically consider
both guided and radiation modes [10]. There are several numerical methods that can be
employed in BPM including Fast Fourier Transform Method (FFT) [16], (FEM [17] and
FDM [18]. In this project, the Finite Difference Beam Propagation Method (FD-BPM)
is employed to investigate light propagation in the silica based pump/signal MUX.
Z
Z+Z
Figure 2.5: The 3D FD algorithm propagates a plane rather than a line along the z-
propagation direction.
34
2.4.1 Beam Propagation Method
Simulation and design works involve approximation [19]. In short, the BPM
employs the FDM to solve the well-known parabolic or paraxial approximation
of Helmholtz equation [20]. BPM was proposed by Fleck et al. (1976) [21] for
solving the scalar Helmholtz equation. However BPM only started to be used in
analyzing and designing integrated optic devices in 1983 by Feit et al. [22].
Although BPM is a solution for paraxial forward propagating wave but it can be
expanded to include effects such as wide angle propagation via Padé
approximation, polarization effect and bi-direction propagation.
As discussed earlier, BPM is a particular approach for approximating the
exact wave equation for monochromatic waves and it can be solved numerically
by FDM [23]. In this section, the main features of BPM and its boundary
condition will be summarized by formulating the problem under restriction of
scalar field (neglect polarization effect) and paraxiality (propagation is restricted
to a narrow ranges of angles) [20]. The three-dimensional scalar wave equation
can be written in the form of Helmholtz equation for monochromatic wave as [4]:
0),,(22
2
2
2
2
2
2
Ezyxnkdz
E
dy
E
dx
E (2.48)
The slowly varying envelope approximation is used to approximate the electric
field ),,( zyxE in the +z direction. In this approximation, ),,( zyxE is separated
into two parts: the axially slowly varying envelope term of ),,( zyx and the
rapidly varying term of )exp( zjkno . Then ),,( zyxE can be expressed as:
35
)exp(),,(),,( zjknzyxzyxE o (2.49)
where the notation of on is a refractive index in the cladding. Substituting the
equation (2.49) into (2.48), we get
0)(2 2222
oo nnk
zknj (2.50)
where 2 is Laplacian equation and is expressed as
2
2
2
2
2
22
zyx
(2.51)
By assuming the weakly guiding condition ( )(2)( 22
ooo nnnnn ), the
equation (2.50) can be rewritten as:
)(2
1 2
o
o
nnjkkn
jz
(2.52)
The above is the wide-angle BPM equation. However, when 02
2
z
, the
equation (2.52) is reduced to:
)()(2
12
2
2
2
o
o
nnjkyxkn
jz
(2.53)
36
This is the para-axial 3D BPM equation. 2D BPM equation is obtained by
omitting the y-direction dependency.
2.4.2 Beam Propagation Method Based On Finite Difference
For simplicity, BPM analysis based on finite difference in this section will be
developed in 2D scalar Helmholtz scalar wave equation which is expressed as:
]),([2
),(2
1 22
2
2
o
oo
nzxnn
kjzx
xknj
z
(2.54)
In equation (2.54), )( 22
onn is not approximated as )(2 oo nnn [4]. Hence,
equation (2.54) can be used in both weakly guiding and strong guiding
conditions. In general, a differential equation of the form:
),(),(2
2
zxBx
zxAz
(2.55)
which can then be can be approximated by FDM as:
zz
m
i
m
i
1
, (2.56)
2
1
1
11
1
2
112/1
2
2
)(
2
)(
2
2
1),(
xxA
xzxA
m
i
m
i
m
i
m
i
m
i
m
im
i
, and (2.57)
37
)(2
1),( 12/1 m
i
m
i
m
iBzxB (2.58)
where x and z imply the compute step in the x- and z-axis respectively.
Meanwhile subscript i and superscript m are the respective grid point along the
x- and z-axis. Comparing equation (2.54) and (2.55), we get:
oknjA
2
1 (2.59)
]),([2
),( 22
o
o
nzxnn
kjzxB (2.60)
Substituting equation (2.56)-(2.60) into equation (2.54), we acquire the
following equations:
m
i
m
i
m
i
m
i
m
i
m
i
m
i
m
i
m
i dqs
11
1
1
11
1 , (2.61)
2/122
222/122 )(2)(4
])[()(2
m
ioo
o
m
i
m
i xknjz
xknjnnxks , and (2.62)
2/122
222/122 )(2)(4
])[()(2
m
ioo
o
m
i
m
i xknjz
xknjnnxkq (2.63)
Therefore when the initial electric field 0m
i is given at z=0, the electric field
m
i at the next propagation step, z=zm can be obtained by computing the equation
(2.61). The FD-BPM based on 3D Helmholtz wave equation can be found in the
following literature [4]. The Transparent Boundary Condition (TBC) [14] is
imposed to FDBPM instead of Dirichlet condition ( 0 ) and Neumann
38
condition ( 0
x
) to reduce reflection from incoming radiation field. TBC
serve as a boundary when the radiation reach the edge of simulation window, it
disappears into the boundary without any reflection.
2.5 Physics of Coupled Waveguide Device
An analysis for the coupling is a critical part to the design of a wide range of
coupled waveguide devices including directional coupler, Mach-Zender interferometer,
bragg grating, ring resonator and modulator. Hence, coupled mode theory is employed
to calculate the coupling along the interaction length and outputs at various wavelengths.
2.5.1 Coupling of Light between Waveguide
The coupling activities are taking place between two adjacent waveguides owing
to the waveguide mode evanescent fields overlapping. When the lights propagate
in a waveguide, small portions of mode or evanescent field propagate into
cladding region as illustrated in Figure 2.6.
(a) (b)
Light
source
Light
source
Figure 2.6: (a) the basic structure of two adjacent waveguide (b) when the lights
launch into an input and propagate down a waveguide, small portions of
evanescent field propagate into cladding region.
39
The intensity of the evanescent field decay exponentially with escalating the
distance into the cladding region [24]. The coupling activities occur between
waveguides only if both waveguides are placed sufficiently close to each other.
The coupling activities are due to the significant overlapping of evanescent field
between one waveguide to the adjacent one [25]. In this condition, the light
energy will be transferred completely from one waveguide to the other in a
periodic manner along the transmission direction [26]. The desired fraction of
light energy can be obtained at a specific length.
2.5.2 Coupled Mode Theory
Generally, the CMT is a method that can be utilized for dealing with the mutual
lightwave interaction between two propagation modes [4]. The behavior of two
modes having mutual coupling is described by the Maxwell’s equations.
Nevertheless a basic understanding of mutual coupling can be acquired from
coupling mode equations [4]:
zi abezBidz
zdA )()(
)( , and (2.64)
zi abezAidz
zdB )()(
)( (2.65)
where )(zA and )(zB are field amplitudes as a function of propagation in z-
direction in the respective waveguide. a and b are the propagation constant in
each waveguide whereas is a coupling coefficient. In this case, we assume two
guided modes propagating in the same direction (+z direction), thus
40
0a and 0b . Equations (2.64) and (2.65) indicate the inter-relationship of
the respective field amplitudes in each waveguide. With the initial condition
1)0( A and 0)0( B which correspond to the one optical input, the solution to
equations (2.63) and (2.64) can be obtained [4]:
zizezA zi
sincos)( (2.66)
zi
ezB zi
sin)( (2.67)
where ab 2 , corresponding to degree of synchronism between the mode
a and b. The parameter defined as 2/122 . From the solution above,
it can be seen that the propagation mode (energy) will transmit back and forth
between two waveguides in a periodic manner. The complex number indicates
the phase change occurring each time the mode is transferred to another
waveguide. It is also apparent seen that the coupling coefficient plays an
important role in coupling activities.
The power flow in waveguide described by 2
)(zA and 2
)(zB and can be
expressed as:
zFA
zA2
2
2
sin1)0(
)( (2.68)
zFA
zB2
2
2
sin)0(
)( (2.69)
41
where 2
2
)/(1
1
F .The minimum distance to achieve a complete
coupling process (maximum power transfer) is defined as the coupling length,
cL given by [4]:
2
mLc , for integer values of m (2.70)
where is the coupling coefficient of the two waveguides. The coupling
coefficient is a parameter used to measure the degree of overlap that occurs
between the evanescent fields of each waveguide [4]. Based on mode
interference phenomena, the coupling coefficient can be acquired by
analyzing both even and odd modes in the waveguides. Therefore, according to
the mode interference phenomena, the minimum distance required for the
complete transfer of light energy from one input waveguide to another
waveguide is:
oe
cL
(2.71)
where e and o are the propagation constant for even and odd modes,
respectively. Hence the coupling coefficient obtained from equation (2.69) and
(2.70) is given by [4]:
42
2
oe
(2.72)
Therefore, the CMT is a crucial and important theory for designing and
optimizing passive optical planar waveguide device in this work.
2.6 Summary
In this chapter, waveguide analysis methods were described. Initially, the chapter gave a
brief description of planar waveguide structure. The buried waveguide is utilized
throughout the work. The light behavior was elaborated in terms of ray optics and
electromagnetic theory. The ray optics approach only can be utilized for qualitative
description. Therefore, electromagnetic theory is applied to explain the relationship
between electric and magnetic field distribution. Some derivations work on obtaining
EM field distribution has been carried out. However the theoretical approaches above is
only used for slab waveguide and there is necessary to use numerical method solver
such as Finite Difference Method to solve the wave equation for buried waveguide.
Finite Difference Beam Propagation Method (FDBPM) was employed to investigate
light propagation in the buried waveguide. Transparent Boundary Condition (TBC) was
imposed to FDBPM to reduce reflection from incoming light. Finally, the Coupled
Mode Theory (CMT) was introduced and discussed. Coupling length, cL give a rough
indication for designing and optimizing the pump/signal multiplexer in the next chapter.
43
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44
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